Answer:
A. 0.25
Step-by-step explanation:
G = Gravitational constant
M = Mass of Earth
m = Mass of space station = Mass of satellite
r = Distance between Earth and object
Centripetal force on Space Station
![F_(ss)=(GMm)/(r^2)](https://img.qammunity.org/2020/formulas/physics/college/o9v1231fe8jqdu4w1vqhz8wbd3z14d3wl4.png)
Centripetal force on satellite
![F_(s)=(GMm)/((2r)^2)\\\Rightarrow F_(ss)=(GMm)/(4r^2)](https://img.qammunity.org/2020/formulas/physics/college/xn7cwj84ctxfmi1as9m2kksn0ej06ms0p1.png)
Divinding the forces we get
![(F_s)/(F_(ss))=((GMm)/(4r^2))/((GMm)/(r^2))\\\Rightarrow (F_s)/(F_(ss))=(1)/(4)=0.25](https://img.qammunity.org/2020/formulas/physics/college/5wp42zxny53mh525ik3iz6sis8lnyfpjri.png)
The ratio of centripetal force acting on the satellite compared to that acting on the International Space Station is 0.25